US2515996A - Propeller blade mounting - Google Patents

Description

` July 18, 1950 P. F. HACKETHAL 2,515,996r

PROPELLER BLADE MOUNTING Filed April 29, 1942 2 Sheets-Sheet l j Ffa/.7

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July 18, 1950 P. F. HACKETHAL Paormm BLADE uouu'rmc.

2 Sheets-Sheet 2 Filed April 29. 1942 Patented July 18, 1.950

UNI-TED fsrA'rEis PATENT OFFICE encaminan. BLADE MOUNTING.

lPal'xl'l'f. Hackethal; Cockeysville, Mdf., assignor to` Everel Propeller' (Sorporatim, Baltimore, Md., ra corpcreation; of Maryland Applieannnnprl ze, 1942 serial No. rinascey however; a plurality of bearing elements areireh i quired" which increases' the wei'ght and'` oost of the propeller: construction. y`Developrn'entsl have beenv made' in which: the' sleeves carrying the Shanks of the. propeller blades are' lrotatably mounted within sockets in the propeller hub em'- plo'ying, ar single bearing. So'rne difficulty has been encountered in properly positioningjthe hearing in the hub and' in` assembling the struc# ture. Also, the loading of thev antifriction bear.'-` ings has notbeen satisfactory due. to the separate external adjustable means for retaining thebearings and the sleeves in the'Y sockets therefor.. V

An object of the present invention is to. Adevise a propeller hub construction which avoids the above pointed' out disadvantages. N y Another object. of this invention is to' provide a propeller construction in which aplurality of blade-shank-receiving sleeves' are' mounted" in sockets. formed' in theJ propeller hub', blocking means are associated with the sockets `to prevent outward movement of the' sleeves, thrust" bear; ings are positioned between the blocking' means and' portionsY of'the` sleeves; and means arepro'- vided' for equally prelbading the bearings.

Another object' ofthis invention is to provide a propeller construction in which. agpluralityof propeller bladeshank-receiving,` sleeves vare rotatably mounted in sockets formed in a huby and pre-loaded bearings areA interposed between'. the sleeves and. blocking means carriedl by, the sockets. to prevent outward movement of .the sleeves from the sockets.` y Still another object ofthi's, invention is to provide a simplified construction'. in which. sleeves carrying propeller blade-shanksfmay be. simply and. effectively mounted` for rotation within sockets provided in a propeller hub;

With these. and othenobjectsin view; the present` invention comprises. the parts and com.- hinationsA herein. described illustrated inf the accompanying drawings.

In the drawings: i

Figure l isV an. axial'. sectional view through .the

hub of' a propeller hub constructed inaccordance. with' the present invention.`

Figure 3 is` still anothersectional View taken on line Ii--Sv of Figure l.

Figure 4 is a further sectional viewy taken on line 4-4' of Figure 1. Y

Figure 51 is a view similar to that of'ligurey 4i illustrating' a modified 'term of' the invention.

Figure 6 is a fragmentary detailed sectional view taken on line E-S of l-igurev 5.

As shown in the drawings, a rotaryl driving member or nulo I ifs provided ar rlange 21 for connectionY withy a drive shaft of an engine'. The rotary` driving member or` hub l hasabore 3 extending' diametrical-ly` or' transversely of the axis` of rotationA thereof". This bore` 3f is shown iin the gures of the drawing asI being enlargedl inter-- mediate its ends but if desired, it mayV have the same diameter througliout,y its extent.v Bore 3 serves as sockets to.V receive sleeves` in which the propeller blade Shanks are mounted?. Adjacent each end oi' thebore, annular grooves 4 are' provided'. These` grooves `are adapted to' receive split` resilient rings 5# which form' part ot the blocking.` means as will be hereinafter described. 1 Mounted in each. end` of the bore13` are sleeves E and 'l which areadapted to receive the Shanks 81 and 9 otV propeller blades. For this purpose, the sleeves are provided with internal threads |l0 which cooperate with threaded portions Il of the shanks-'and 9; The outer ends of' the sleeves 6 and 1 are provided with. cuffs i12 having a plurali-ty of axially extending' slits.V I3;` and about which extend clamping elements. M which, after the propeller' bladeshave been threaded into. the sleeves,- serve4 to clamp the same into the said sleeves' against' relative rotation. Aswill be noted from the drawings, the inner ends; of the sleeves 6: and. 1. are/provided? with outwardly' extending flanges l5 surroundingl the cylindrical portionsdoil thev sleeves.` Positioned on:` thel sleeves' in'. juxtaposition tothe. circum` ferentiali arnges 't5 are; anti-friction. .beaming members which. compriseI an inner raceV IBI, an outer'xrace |12, and a series of balls l carried; in a'A retaining. ring: t9 and interposed between the racesf L6 and lfxl. These: anti-friction bearing means.- are: of? they thrust? typef and' are. designed to prevent' outward radial' movement of the sleeves 6@ and 1 from theirA sockets which. are fomned by the' bore 3..

interposed'. 'between the outer' race I lr ofth bearing means and! the split ring `5 is an annular member 20 which is of an external diameter substantially equal to that of the portion of the bore 3 adjacent the ends thereof. The inner diameter of said annular member 20 is slightly larger than that of the sleeves 8 and 9 and sealing means in the form of a leather washer or another suitable element 2| is carried by the inner portion of said annular member 20 to effect a seal between the Vannular member 20v and the sleeves 6 and 1.

It will be noted that adjacent the outer end of the annular member 20 its external diameter is reduced to form a shoulder which receives and cooperates with the split ring 5 to retain said split ring in the groove 4.

Since in rotation there is considerable centrifugal force exerted on the blades of the propeller, the primary force to be considered in connection with the mounting of the sleeves 6 and 1 in the sockets provided therefor is that of radial outward movement. Consequently, during rotation theflange I5 of the sleeves will Acompress the anti-friction bearing between the same and the annular member 20 which is retained against outward movement by the split ring 5.

It is desirable, however, that said bearing be loaded at all times, even when the propeller is stationary. For this purpose, the present invention provides means between the inner ends of the sleeves 6 and 'l for mutually forcing said sleeves outwardly away from each other and thereby maintaining a lload on the anti-friction bearings at all times. As shown in the drawings, the inner end of the sleeve 6 is provided with a recessed portion to receive an anti-friction bearing 22 which in turn receives the reduced end of an internally and externally threaded tubular member 23.

The inner end of the sleeve 1 is recessed to receive an annular internally threaded annular member 24 which receives the externally threaded portion of the tubular member 23. As clearly shown in the drawings, the threaded portion of the tubular member 23 is provided with l an axial slit 25 to render the same radially or circumferentially resilient. Mounted within the internally threaded portion of the tubular member 23 is a plug 26. This plug is of tapered formation and the internally threaded portion of the tubular member 23 is of similar formation so that when said plug 26 is threaded into the tubular member 23, the slit threaded portion of the latter will be expanded. This serves to lock or x the tubular member 23 and the annular member 24 against relative rotation.

In assembling the hub and sleeve construction as illustrated in the drawings, the anti-friction bearing means are positioned on the sleeves together with the annular members 20 and the sleeves with the associated members are then inserted into each end of the bore 3. The tubular member 23 is screwed into the annular member 24 sufiiciently to draw the sleeves 6 and 'l together to permit the split rings 5 to be easily inserted in position in the grooves 4 provided in the bore 3. After positioning the sleeves Gand 1 in the bore 3 and mounting the split rings 5 in place, 'the tubular member 23 and the annular member 24 are unscrewed to such an extent as to exert a predetermined outward opposing vforce on the inner ends of the sleeves which tends to equally pre-load the anti-friction bearings interposed between the flanges I5 of the sleeves 6 and 1 and the means for blocking outward movement of the sleeves from the sleeve sockets or ends of the bore 3. After this adjustment has been made, then the plug 26 is screwed into the tubular member 23 to enable the threaded portion of the said tubular member to expand into tight engagement with annular member 24 so that said members will be locked against relative rotation. To facilitate adjustment of the tubular member 23, it is provided with a slot 2l and for adjusting the position of the plug 26, the latter is provided with a hexagonal socket 28.

Instead of the split ring 5, it is also within the concept of the present invention to employ a segmental ring to retain the annular member 20 within the ends of the bore. As shown in Figure 5 of the drawings, a ring of three or more segmental parts 29 ymay be inserted in the grooves 4 in the inner walls of the bore 3. While a three part ring will not of its own volition be maintained within the grooves 4 in the wall of the bore, nevertheless, after such a member has been assembled and pressure exerted on the inner ends of the sleeves to load the bearings, the annular members 20 will have their reduced portions enter into engagement with the inner peripheral portions of said segmental ring members and thereby serve to retain the latter within the grooves 4 in the wall of the bore 3.

It will be appreciated from the foregoing description that the present invention provides a simple propeller hub construction in which the parts may be easily and effectively assembled and in which the anti-friction bearing means carrying the outward thrust due to centrifugal force in rotation of the propeller are equally preloaded. By pre-loading the anti-friction bearings which carry the outward thrust of the propeller blades during rotation of the propeller, the deections between the rotary parts of the bladeshank-carrying sleeves and the sockets in which they are mounted are greatly reduced so that the life of the anti-friction bearings and the other movable parts of the propeller hub assembly are greatly increased.

I claim:

1. In a propeller having a plurality of blades, a rotary driving element having blade-shank-receiving sockets formed therein, blade-shankreceiving sleeves mounted in said sockets, thrustbearing means carried by said sleeves, blocking means engaging said bearing means for limiting outward displacement of the sleeves from said sockets, threadedly interengaged adjustably expansible means extending between the sleeves and equally urging said sleeves outwardly of said sockets to equally pre-load said bearing means, and means forxing said expansible means in adjusted positions.

2. In a propeller having a plurality of blades, a rotary driving element having blade-shank-receiving sockets formed therein, blade-shank-receiving sleeves mounted in said sockets, peripheral ilanges on Said sleeves, anti-friction bearing means on said sleeves in engagement with said anges, means engaging said bearing means to block outward displacement of the sleeves from saidsockets, an internally screw threaded element engaging vthe inner portion of one sleeve, and an externally screw threaded element engaging the inner portion of another sleeve, said screw threaded elements being interengaged and equally urging the sleeves associated therewith outwardly of their sockets to equally pre-load the bearing means on said sleeves.

v 3. In a propeller )having a plurality of blades, a rotary driving element having blade-shank-receiving sockets formed therein, blade-shank-receiving sleeves mounted in said sockets, peripheral flanges on said sleeves, anti-friction bearing means on said sleeves in engagement with said flanges, means engaging said bearing means to block outward displacement of the sleeves from said sockets, an internally screw threaded element engaging the inner portion of one sleeve, an externally screw threaded element engaging the inner portion of another sleeve, said Screw threaded elements being interengaged and equally urging the sleeves associated therewith outwardly of their sockets to equally pre-load the bearing means on said sleeves, and means for locking the interengaged screw threaded elements in adjusted positions.

4. A propeller ycomprising a rotary driving member having a bore extending diametrically therethrough transversely of the axis of rotation, a blade-shank-receiving sleeve positioned in each end of said bore, anti-friction bearing means mounted on each sleeve and fixed thereon against relative inward axial movement, blocking means associated with the end portions of said bore to engage said bearing means and block outward movement of said sleeves adjustably expansible, means connecting the inner portions of each sleeve for forcing the sleeves outwardly and urging the bearing means against the lblocking means with equal predetermined force, said bore having an annular groove in its wall adjacent each end thereof and said blocking means being in the form of a split ring mounted in said groove and extending radially inwardly of said bore.

5. A propeller comprising a rotary driving member having a bore extending diametrically therethrough transversely of the axis of rotation, a blade-shank-receiving sleeve positioned in each end of said bore, anti-friction bearing means mounted on each sleeve and fixed thereon against relative inward axial movement, blocking means associated with the end portions of said bore to engage said bearing means and block outward movement of said sleeves adjustably expansible means connecting the inner portions of each sleeve for forcing the sleeves outwardly and urging the bearing means against the blocking means with equal predetermined force, said bore having an annular groove in its wall adjacent each end thereof, said blocking means comprising an annular member having an external diameter substantially equal to that of the bore with a portion of reduced external diameter at its outer end, and ring segments positioned in said grooves and retained therein by the reduced outer end of the annular member.

6. A propeller comprising a rotary driving member having a bore extending diametrically therethrough transversely of the axis of rotation, a blade-shank-receiving sleeve positioned in each end of said bore, anti-friction bearing means mounted on each sleeve and xed thereon against relative inward axial movement, blocking means associated with the end portions of said bore to engage said bearing means and block outward movement of said sleeves, an internally threaded member carried by the inner portion of one sleeve, an externally threaded member carried by the inner portion of the other sleeve, said threaded members being threadedly connected and adjusted for forcing the sleeves outwardly and urging the bearing means against the blocking means with equal predetermined force.

7. In a propeller having a plurality of blades, a rotary driving element having blade shank receiving sockets formed therein, blade shank receiving sleeves mounted in said sockets, peripheral flanges on said sleeves, anti-friction bearing means on said sleeves in engagement with said anges, means fixed at a predetermined distance from the axis of said rotary driving element and cooperating with the flanges for blocking outward displacement of the blades from the sockets and means interposed between the inner ends of said blade Shanks for pressing the blade shanks radially outwardly, said last mentioned means including a part engaging the inner end of one blade shank, a, part including an anti-friction bearing engaging the inner end of another blade shank, means for adjusting said parts relative to each other to vary the pressure exerted thereby on the inner ends of said blades, and means for fixing said parts in their adjusted positions.

8. An adjustable variable pitch air screw comprising a hub provided with means for mounting it upon a drive shaft for rotation about the axis of the drive shaft, said hub being provided with radial recesses, a blade receiving sleeve freely rotatably mounted in each of said recesses, a blade having its shank mounted in each of said sleeves, cooperating means on each sleeve and the hub for limiting outward movement of each of said sleeves in the recess in which lt is mounted, expansible means interposed between the inner portions of said sleeves and engaging said sleeves for pressing the same radially outwardly of said recesses, said expansible means including cooperating elements adjustable relatively to each other, and means for fixing said elements relative to each other in adjusted positions.

PAUL F. HACKETHAL.

REFERENCES CITED The following references are of record in the file of this patent:

UNITED STATES PATENTS Number Name Date 1,849,012 Lougheed Mar. 8, 1932 1,907,504 Chilton May 9, 1933 1,956,055 Wiegand Apr. 24, 1934 1,973,573 Lougheed Sept. 11, 1934 2,109,696 Hackethal Mar. 1, 1938 FOREIGN PATENTS Number Country Date 476,972 Great Britain Dec. 20, 1937 485,102 Great Britain May 13, 1938 486,614 Great Britain June 8, 1938 727,628 France June 21, 1932

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